发明授权
US09322293B2 Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe
有权
涡轮喷气通风管,一个这种管道的安装方法和一个这样的管道的涡轮喷气发动机
- 专利标题: Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe
- 专利标题(中): 涡轮喷气通风管,一个这种管道的安装方法和一个这样的管道的涡轮喷气发动机
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申请号: US13636802申请日: 2011-03-28
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公开(公告)号: US09322293B2公开(公告)日: 2016-04-26
- 发明人: Michel Gilbert Roland Brault , Philippe Pierre Vincent Bouiller
- 申请人: Michel Gilbert Roland Brault , Philippe Pierre Vincent Bouiller
- 申请人地址: FR Paris
- 专利权人: SNECMA
- 当前专利权人: SNECMA
- 当前专利权人地址: FR Paris
- 代理机构: Oblon, McClelland, Maier & Neustadt, L.L.P.
- 优先权: FR1052239 20100326; FR1052242 20100326
- 国际申请: PCT/FR2011/050676 WO 20110328
- 国际公布: WO2011/117560 WO 20110929
- 主分类号: F01D25/18
- IPC分类号: F01D25/18 ; F16L37/14 ; F16L21/08
摘要:
A venting pipe used to guide a gas stream in a turbojet including at least one hollow rotary shaft inside which the pipe is mounted, the pipe extending generally along an axis. The pipe includes at least two pipe segments configured to be aligned longitudinally and assembled to one another while retaining a degree of freedom in relative translation thereof, at least one of the segments including a deformable mechanism configured to deform radially as the pipe segments are tightened against one another in the shaft of the turbojet, to bear on the shaft. The pipe structure facilitates mounting of the pipe.
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